Method for identification of different states of water, and sensor arranged for the method

Abstract: The invention relates to a sensor arrangement for identification of different states of water on the surface of a structure (1). The sensor arrangement (2) comprises at least one longitudinal sensor element (2) manufactured of a material conveying acoustic oscillation and a transmitter-receiver unit (3) coupled at the ends of the sensor element (2) for transmitting acoustic oscillation, preferably oscillation in the ultrasonic range, to the sensor element (2) and for receiving the response of the transmitted oscillation. The transmitter-receiver unit (3) is arranged to transmit oscillation and to receive the response of the transmitted oscillation from both ends (6, 7) of the sensor element (2). The invention relates also to a method using the sensor arrangement.

Description: The invention relates to a method for identification of different states of water on the surface of a structure, upon which a sensor element has been placed, the sensor element being made of a material conveying acoustic oscillation, whereby the sensor element is connected at its ends to a transmitter-receiver unit. The invention relates also to a sensor arrangement for identification of different states of water on the surface of a structure, upon which at least the sensor element of the sensor arrangement is placed, whereby the sensor arrangement comprises: at least one longitudinal sensor element made of a material conveying acoustic oscillation and a transmitter-receiver unit coupled at the ends of the sensor element, for transmitting acoustic oscillation, preferably oscillation effective in the ultrasonic range, and for receiving the response of the transmitted oscillation. As to the prior art in the field, reference is made to the publication GB-1,117,664 which discloses a method according to the preamble of claim 1. The solution disclosed in this publication cannot, however, be used for reliable identification of, particularly, the formation of ice on the structure upon which the sensor arrangement is placed, especially under demanding conditions. In particular, when using this prior art approach, it is impossible to distinguish between the different states of water. Further, it is impossible to locate a change in the state particularly within the range of placement of the sensor arrangement. It is an aim of the present invention to present a method for achieving particularly precise identification of the different states of water from a medium, e.g. the atmosphere or water, in which the sensor arrangement is placed, within the measuring range of the sensor arrangement, detection of a local change in the state, as well as a continuous possibility for checking the working order of the sensor arrangement. For achieving these aims, the method of the invention is primarily characterized by the features of the second part of claim 1. It is also an aim of the invention to present a sensor arrangement which is primarily characterized by the features of the second part of claim 6. The measurement carried out by the method and by the sensor arrangement is thus based on measuring the attenuation of the oscillation generated in the sensor element, the oscillation penetrating different states of water in the measuring range of the sensor element. The frequency of the oscillation to be generated is preferably an ultrasound outside the hearing range of the human ear. The oscillation is transmitted by the transmitter-receiver unit preferably in pulse form or pulse burst form. The amplitude of this oscillation is reduced, if the water in the measuring range of the sensor arrangement begins to freeze via slush formation. The response of the transmitted oscillation received as the measuring result can be scaled e.g. in such a way that the measuring result obtained for water in the measuring range has a numerical value of about 1.0, for slush about 0.6 and for ice about 0.2 to 0.0. When, according to the invention, oscillation is transmitted to the sensor element in both directions and received from both directions, it is possible to verify e.g. a local change of state exactly in the measuring range of the sensor arrangement. Thus the front edge of the local change of state (i.e. the edge receiving the oscillation transmitted from the transmitter-receiver unit in said transmitting direction) indicates a first response (return reverberation) in the direction opposite to the transmitted oscillation along the sensor element back to the transmitter-receiver unit. The time taken in this operation can be measured and multiplied with the travelling speed of the pulse, e.g. 5000 m/s, to obtain the distance to-and-fro. On the other hand, a local change of state locks the sensor element in the structure either directly or by means of a support according to one embodiment of the invention, whereby the oscillation at the change of state is transferred to the structure whose surface is monitored. Thus, the second response of the oscillation can be received at the end of the sensor element opposite to the transmitting end. Consequently, the time spent between sending the oscillation and receiving either or both of the responses is shorter than the time required for penetrating the sensor element in a normal situation. These measurements can be made at both ends of the sensor element at certain intervals as automatic pulses or pulse bursts in opposite directions. By the method presented above, the beginning of the change of state of water is determined in a reliable way, and the location is thus defined on the basis of the time interval between sending the oscillation and receiving the response of the same. The frequency of the oscillation exceeds 20 kHz up to 300 kHz. It is important to choose the frequency so that it exceeds the frequencies of free vibration in the structure 1. Particularly in a case when the sensor element of the sensor arrangement is damaged and broken, the oscillation will not penetrate the sensor element; thus, the only available response is the response of the transmitted oscillation returned from the cut-off point to the transmitting end of the sensor element, which has substantially retained its amplitude. By the method and sensor arrangement of the invention, it is possible to locate the cut-off point and also to check it by controls in both directions in the sensor element by measuring the time difference between the oscillation leaving and returning from both ends of the sensor element with a known travelling speed of the oscillation. Further, some advantageous embodiments of the method and sensor element of the invention are presented in the appended dependent claims. The invention will be illustrated in more detail in the following description with reference to the appended drawings. In the drawings, FIG. 1 is a schematic general view of a total system using the sensor arrangement of the invention, Fig. 2 shows two alternatives of a first embodiment of the sensor arrangement placed on the surface of a wing or a rotor, Fig. 3 is a schematic view of a second embodiment of the sensor arrangement, where the sensor element is pre-installed on a support with the shape of a longitudinal form part fixed in a structure, different states of water being identified on the surface of the same, whereby partial figure 3a shows a cross-sectional view of said embodiment in a larger scale, Fig. 4 is a schematic perspective view of a third embodiment of the sensor arrangement of the invention, Fig. 5 is a schematic perspective view of a fourth embodiment of the sensor arrangement of the invention, Fig. 6 is a schematic perspective view of a fifth embodiment of the sensor arrangement of the invention, Fig. 7 is a cross-sectional view of an embodiment of a lead-in arrangement useable in embodiments of sensor arrangements according to the invention, Fig. 8 is a schematic perspective view of part of an alternative implementation with reference to the second embodiment showin in Fig. 3, Fig. 9 shows the use of a combination of several embodiments of the sensor arrangement in connection with a ship, Fig. 10 shows the use of a combination of some sensor arrangements according to above-mentioned embodiments, and Fig. 11 shows schematically an embodiment of sensor arrangement according to the invention in an arrangement for measuring road surface conditions. Figure 1 shows a general view of a total system in which one or several sensor arrangements of the invention can be applied for identifying different states of water. In Fig. 1, reference number 1 denotes to a structure, a surface structure or a support structure, the thread-like or band-like sensor element 2 of the sensor arrangement being placed upon the same. When water or different states of water are present on the surface of the structure 1, the sensor arrangement can be used for identifying the state of water in question. The capacity of the sensor arrangement to differentiate between the different states of water will remain even if chemicals of various types, such as glycol, salt, etc. were added into the water. The sensor element 2 is connected with the transmitter-receiver unit 3. As shown in Fig. 1, the sensor element 2 is arranged to form a loop, whereby the transmitter-receiver unit 3 is a uniform unit, i.e. the same unit acts as transmitter and receiver (either a single device or two devices integrated together), both ends 6, 7 of the sensor element 2 being fixed thereto. In most embodiments, the loop-like sensor element 2 is, to secure the many uses, advantageously placed in a functional manner in the frame 1, the loop form of the sensor element 2 being, at least on part of the length of the sensor element 2, a parallel part 2a, in which the sections of the sensor element 2 are substantially aligned and at a distance from each other, whereby e.g. freezing will "close" the loop form of the sensor element by combining the zones e.g. at a point J' in Fig. 1. The transmitter-receiver unit 3 operates as a local control unit which is electrically (line 4a) connected with a central control unit 4, which is, in turn, electrically connected (line 5a) with a monitor device, such as a display unit 5. For example on the basis of visual information from the display unit 5, the structure 1 can be subjected to operations, e.g. melting or de-icing either by liquid spraying (glycol, salt, etc) or by electric heating. The operations T can be either carried out manually or automated to be part of the total system controlled by the central control unit 4 (line T 1 to the operational unit TY). In case of local ice formation at the point J of the sensor element 2, the sensor arrangement of the invention operates in the following manner. The transmitter-receiver unit 3 transmits oscillation in pulse form or pulse burst form in a first direction (e.g. counterclockwise) through the sensor element. The direction of transmission is shown by arrow V 1 in Fig. 1. Thus the transmitter-receiver unit 3 receives the response of the oscillation V 1 at the first end 6 of the sensor element 2 (transmitting end of the oscillation V 1 ). This response VV 1 is reflected from the first front edge J 1 of the ice formation J. On the other hand, the oscillation V 1 transmitted from the first end 6 is also reflected in the structure 1 (or in the support, cf. Figs. 3 and 7), whereby it, having passed the ice formation J, is transmitted in part back to the sensor element 2, whereby the second response VV 2 is received at the second end 7 of the sensor element. A corresponding operation is carried out also by transmitting the oscillation from the second end of the sensor element as an oscillation V 2 , whereby the responses of the oscillation V 2 are received in a corresponding manner as shown by arrows VV 3 and VV 4 , whereby the second edge J 2 of the ice formation can be determined. The above-mentioned measuring signals are transmitted by the transmitter-receiver unit 3 to the central control unit 4 provided with a calculation programme for detecting and locating the ice formation J in the range of the sensor element 2 numerically. The ice formation J can thus be located very precisely within the range on the basis of the position information received on its edges J 1 and J 2 . Information on the ice formation J is received at the display unit 5, and possibly either manual or automatic measures T are taken after detecting the ice formation. Consequently, the above-described embodiment is based on the following steps: A) acoustic oscillation V 1 is transmitted to the sensor element 2 by the transmitter-receiver unit 3 at the first end 6 of the sensor element 2, whereby B) the first response VV 1 of the acoustic oscillation V 1 transmitted at the first end 6 and possibly reflected back from the measuring range of the sensor element 2 is received by the transmitter-receiver unit 3 at the first end 6 of said sensor element 2, the first response indicating a change in the state of water, whereby C) the second response VV 2 of the acoustic oscillation V 1 transmitted by the first end is received at the second end 7 of the sensor element 2 of the transmitter-receiver unit 3, whereby D) the steps A to C are carried out so that acoustic oscillation V 2 is transmitted by the second end 7 of the sensor element 2, whereby the responses VV 3 , VV 4 of the acoustic oscillation V 2 transmitted to the sensor element 2 are received according to steps B and C, respectively, whereby E) the steps A to C are repeated at certain intervals by alternating the transmitting end 6, 7 of the acoustic oscillation V 1 , V 2 , if necessary, and whereby F) the information from the transmitted oscillations V 1 , V 2 and their responses VV 1 , VV 2 ; VV 3 , VV 4 is used for calculating the state of water in the measuring range of the sensor element 2. Figure 2 shows the first embodiment of the sensor arrangement in two alternatives. They are placed on a wing of an aircraft or on a rotor, e.g. a rotor of a wind power station, functioning as the structure 1. The left-hand alternative is intended to be placed on a surface 8a of a wing or rotor 8 subjected to icing, and the right-hand alternative is intended for those purposes where the sensor arrangement is intended to measure the situation of the leading edge of the wing or rotor in addition to the surface 8a and thus to overlap said leading edge 8b. In both alternatives, the sensor element 2 has a loop form and is intended to be placed directly on the surface of the wing or rotor functioning as the structure 1. For achieving the loop form, the sensor element penetrates (lead-ins L 1 , L 2 , L 3 , L 4 ) four times the surface of the structure 1, each lead-in being provided with an insulating and clamping device, whereby the sensor element 2 is tightened against the outer surface of the wing or rotor, one embodiment being shown in Fig. 7. The sensor element 2 is thus placed on the first (outer) surface, whereby the transmitter-receiver unit 3 is placed on the side of the second surface of the structure 1, underneath the outer surface. The loop form of the sensor element 2 is achieved by connecting the suitably parallel measuring zones 2a of the sensor element 2 to each other by a connection 2b of the material of the sensor element, placed between the lead-ins L 2 and L 3 underneath the surface 8a. After the lead-ins L 1 and L 4 , the connections 2c and 2d connect the sensor element to the transmitter-receiver unit 3. In the case of an aircraft wing, it is advantageous to place the sensor element to overlap the interface of the fuel tank, whereby it is possible to monitor the situation on the surface 8a both against the fuel tank and against a point where there is no fuel on the side opposite to the surface 8a. The interface of the fuel tank is referred to by the index 8c in Fig. 2. Figure 3 shows an embodiment of the sensor arrangement where the sensor element 2, preferably pre-installed and tested, is placed on a support 9, through which the sensor element 2 is at least partly fixed on the first surface of the structure 1, e.g. a wing of an aircraft or a rotor. The support 9 is a longitudinal, flat form piece, its first bottom surface 10 being provided with fixing and support means 9a for fixing the sensor element 2 on the support 9. The fixing and support means 9a providing the loop form of the sensor element 2 are arranged on the first surface of the support 9 in a way that at least part of the length of the sensor element 2 forms a parallel part 2a where the sections of the sensor element are aligned, at a distance defined by the fixing and support means 9a of the support. The second bottom surface 11 is intended to be placed against the first (outer) surface of the structure 1. The lead-ins L 1 and L 4 and the connections 2c and 2d can be arranged in a manner shown in Fig. 2. The support can be fastened to the structure e.g. by screws 12 or by glueing. The sensor arrangement shown in Fig. 3 can be used on the outer surface of a wing or rotor in a manner similar to the embodiments of Fig. 2. The support 9 is thus bent to correspond to the shape of the outer surface of the structure 1, e.g. to overlap the stagnation point. The sensor element 2 and the support 9 form a strong structural entity which can be used e.g. to cover such sections of a wing where no screws can be fastened or which cannot be fixed in another way. (The whole structure is mounted in a pre-installed form and tested against its support.) Particularly Fig. 8 shows an alternative support, upon which the sensor element 2 is pre-installed to be ready for fixing to the structure 1. Thus the longitudinal form piece forming the support 9 is provided at its both longitudinal side surfaces with parts 13 protruding from the frame of the support 9. Further, the support 9 is formed of two pieces 9b, 9c to be fixed on top of each other. The protruding parts 13 are provided with grooves or the like in the longitudinal direction of the support 9 for receiving the sensor element 2. The protruding parts 13 are placed at a distance from each other in the longitudinal direction of the support 9, whereby free sections 13a are formed in the longitudinal direction of the sensor element 2 at the side of the support between the protruding parts 13, the sensor element 2 being exposed to fresh air at said point. Alternatively, or additionally, free sections 13a' may be provided between the protruding parts 13, these free sections 13a' corresponding to a space in the upper support piece 9b, the lower support piece remaining continuous. In the latter case too sensor element 2 is exposed to fresh air. By changing the thickness of the lower support piece 9c it is possible to control the distance of the sensor element 2 from the structure 1. If needed, the protruding parts 13 can be provided with insulators for insulating the sensor element 2 from the support 9. In this embodiment, the protruding parts 13 and the grooves in them form the fixing and support means 9a for the sensor element 2. The support 9 is further provided with holes 12 for the screw fastening. Figures 4 and 5 show two other embodiments of the sensor arrangement. Figure 4 shows a support formed of a plate 14 or the like provided with fixing means 14a, such as holes, for fastening by screws, rivets or the like, and of a bar-like structure 15 protruding from the plate 14, the outer surface of the structure 15 being encircled by the first section 2' of the sensor element 2 penetrating the plate 14 or the like and extending up to the upper end of the bar-like structure 15. The second section 2'' is led through the inner hole 15c penetrating the bar-like structure and parallel to its longitudinal direction to the transmitter-receiver unit 3. Figure 5 on the other hand shows an embodiment in which the bar-like structure 15 is U-formed, whereby the ends of the branches 15a, 15b of the U-form are provided with plates or the like 14' and 14'' for fixing the sensor arrangement to the structure in a manner such as in Fig. 4. The sensor element 2 is threaded around the U-form, the threading beginning after the clamp 2c extending from the transmitter-receiver unit 3, whereby the sensor element penetrates through the plate 14' or the like, passes from the first branch 15a to the second branch 15b of the U-form, penetrates the plate 14' and is connected with the transmitter-receiver unit 3 by a connection 2d. Figure 6 shows a fifth embodiment of the sensor arrangement of the invention, with an element 15d formed as part of the actual bar-like structure 15 and fastened to the rear part 15e e.g. by glueing or by screw fastening, particularly to form the leading edge of a wing. The element 15d comprises, in addition to the section 2e of the sensor element 2 on its surface, also a heating resistance arrangement 16 intended for ice melting (e.g. two heating resistances in the longitudinal direction of the sensor element 2). This embodiment is provided e.g. with a plate 14 or the like as shown in Figs. 4 and 5 and with corresponding fastening means 14a forming part of the support. Consequently, the support comprises, like the element 15d, also a rear part 15e protruding from the plate 14, whereby the parts 15d and 15e form together the bar-like structure 15 which has the form of a wing profile when seen in a cross-section perpendicular to its longitudinal direction. The section 2e of the sensor element 2 is arranged against the stagnation point of the wing profile and aligned with it on the outer surface of the bar-like structure 15. The sensor element 2 is led to its section 2e on said outer surface inside the bar-like structure 15 (section 2f). This section 2f of the sensor element 2 is connected at its ends to the transmitter-receiver unit 3. The heating resistance arrangement 16 in the front part of the wing profile is controlled by the central control unit 4 particularly in a manner shown in Fig. 11. The embodiment of Fig. 6 is particularly intended for use in connection with an aircraft and to be placed in the frame of the aircraft for monitoring possible formation of ice during the flight. The solution corresponding substantially to the embodiment of Fig. 6 can also be applied by the structure of Fig. 2, whereby the sensor element 2 is led in alignment with the stagnation point of the wing or the rotor on at least part of the length of the wing or rotor. Figure 7 shows one embodiment for applying the lead-in arrangement shown in the previous figures with the general indexes L 1 -L 4 . The structure 1 is provided with a hole R, through which the sensor element 2 is led from the side of the first surface to the side of the second surface of the structure 1. The hole has an insulation structure E for preventing leaks through the hole R. On the side of the second surface, there is a clamping device KR which is fastened to the structure 1 and comprises a support plate TL protruding diagonally from the second surface substantially at the hole R and provided with a longitudinal slot PR. The sensor element is fastened with a slide clamp LR which is arranged to be movable in the longitudinal direction of the slot PR and locked against the support plate TL with a locking screw L. The slide clamp LR is fastened with the sensor element with a fastener K. The sensor element 2 can thus be tightened by transferring the slide clamp LR in the longitudinal direction of the slot PR onto the first surface of the structure 1, the connections 2b-2d being free from the clamping effect. In general, the clamping device thus comprises a first part (i.e. the support plate TL) and a second part (i.e. the slide clamp LR), of which the first one is fastened onto the second, or inner, surface of the structure 1 and the second one is fastened to the sensor element 2. The first and second parts are arranged to be movable in relation to each other for clamping the sensor element 2. The parts are locked in relation to each other by a locking device (i.e. the locking screw). This construction can be modified in its structure to a great extent. Figure 9 shows an application of the total system in connection with a ship. Thus three sensor arrangements are placed on one hand in the mast M of the ship and on the other hand in connection with the radar TU and the funnel S, for monitoring the situation at points important for the functions of the ship in a manner shown particularly in Fig. 1. Figure 10 shows an embodiment of the invention, in which different embodiments of the sensor arrangement of the invention are used for multiple measuring of appearance of different states of water at several different locations. In the total system, a sensor arrangement A (Fig. 4) is used for monitoring the freezing of supercooled water, a sensor arrangement B is used for monitoring the situation at ground level by operating as a bottom describing e.g. a road surface (e.g. an embodiment of Fig. 3), and thirdly sensor arrangements C and D e.g. in connection with a rotor of a wind power station and/or in connection with a mast construction are used for monitoring the freezing of a fog cloud. The sensor arrangements according to the embodiment C can be constructed as shown e.g. in Figs. 2 and 3, and the sensor arrangements of the embodiment D can be similar to those shown e.g. in Figs. 4 and/or 5. All these sensor arrangements are connected with the central unit 4 for carrying out further measures by means of the display 5 and the operational unit TY. Further, Fig. 11 shows an embodiment of the sensor arrangement of the invention, where the sensor arrangement functions as part of the total measuring system in such a way that the sensor arrangement, at least the sensor element 2, is provided in a formed piece functioning as a support provided with e.g. electrically operated heating and cooling units 16 and 17 as well as one temperature-measuring sensor 18 embedded in the same. These parts are connected, in addition to the transmitter-receiver unit 3 of the sensor arrangement to the central control unit 4 for monitoring the appearance of the states and temperature of water under road conditions, e.g. on the surface of a main road, and connected with e.g. a display 5 for informing automobile drivers. As shown in the above examples, it is possible to install the sensor arrangement in different structures by electing a suitable embodiment for each structure in such a manner that the sensor arrangement does not disturb the operation of the structure. Examples of structures in which the sensor arrangement of the invention can be applied, are given in the following: Aircraft wings, stabilizers, engine air inlets, helicopter rotors, rotors of wind power stations, ship structures, masts, davits and corresponding systems, radar and other antennas and mast structures, other vehicles and passages of the same. By combined use of different embodiments of sensor arrangements, it is possible to measure several different conditions of the environment simultaneously. The arrangements can be connected with one and the same central unit, as shown particularly in Figs. 9 to 11. Thus the central unit can be used to control the required operations, e.g. visual information and/or melting measures etc. The total system can also be utilized by programming the central unit with logistics providing information for drawing various conclusions or deleting irrelevant information. Particularly the embodiments of the sensor arrangement with the sensor element placed on a support (Figs. 3 to 6 and 8) are intended for uses where the sensor element is submitted to various mechanical stresses, e.g. in connection with deicing on the wing of an aircraft or removal of ice upon heating the structure, e.g. the rotor of a wing power station, when the ice to be removed generates forces tending to detach the sensor element. It is obvious that the construction and choice of material of the support can also be used to control the movement of the pulse from the sensor element to the support and/or to the structure in connection with the support and back to the sensor element for determination of the front and back edges of the local change of state. As described above particularly in connection with the embodiment of Figs. 6 and 11, the structure 1 and/or the support can also be provided with a heating and/or cooling unit for heating the structure 1 and/or the support and thus for melting the ice in connection with the structure 1 and/or the support, and in case freezing is still going on after heating, by repeating the melting process at necessary intervals it will be detected that the water is found as ice under said measuring conditions and that said situation is still going on. The melting element can also be placed in the support e.g. in connection with the frame of the support 9, immediately against the head parts of the protruding parts 13 in the longitudinal direction of the support, as shown in the structure of Fig. 8. Particularly in the embodiment of Fig. 11, it is advantageous that the support is formed e.g. as a piece simulating the conditions of a road with an asphalt coating and being placed away from the actual traffic road for preventing damage to the sensor system and the support. The sensor arrangement can also be used for measuring other physical quantities, such as the temperature of the sensor element, whereby the measurements of this kind can be made for purposes of the functioning of the total system, e.g. for monitoring the working order of the sensor element. With particular reference to the embodiment of Fig. 2, the sensor element can be installed directly in various structures, such as aircraft wings, by lead-in arrangements not dampening ultrasound, whereby the sensor element can be transferred to extend inside the structure, i.e. on the side of the inner surface. Thus a measuring range consisting of several measuring range parts is obtained by using a common sensor element for all measuring range parts. The lead-in part can comprise an insulating part, by means of which the sensor can be clamped on the surface of the structure 1 (cf. Fig. 7). The clamped sensor element is thus pressed tightly against said surface and it endures mechanical stresses, such as deicing, wind, etc. The sensor element according to the invention can also be formed of several elements, as is usually needed particularly for the connection 2b in the embodiment of Fig. 2. The sensor wire can also be extended by a separate extension piece. This will facilitate the installation of the sensor wire or its repair upon breaking of the wire. With reference to the above presentation, the sensor arrangement according to the invention has various applications as to its installation and use. The sensor arrangement can be applied either when fully mounted in place, or the sensor arrangement can be pre-installed on a support and tested under production conditions. In addition to the measuring results of the sensor arrangement, the total system can be used to combine several physical occurrences and information related to the change of state, including time, temperature, false alarm, operations by the user, etc.

Claims: Method for identification of different states of water on the surface of a structure (1), upon which a sensor element (2) has been placed, the sensor element being made of a material conveying acoustic oscillation, whereby the sensor element (2) is connected at its ends to a transmitter-receiver unit (3), characterized in that acoustic oscillation (V 1 , V 2 ) is transmitted by the transmitter-receiver unit (3) alternately to each end (6, 7) of the sensor element (2) and the corresponding response (VV 1 , VV 2 ; VV 3 , VV 4 ) is received by the transmitter-receiver unit (3) at both ends (6, 7) of the sensor element (2). Method according to claim 1, characterized in that the oscillation is transmitted as oscillation in the ultrasonic range in pulse form and/or pulse burst form, whereby the frequency of the oscillation is 20-300 kHz. Method according to claim 1 or 2, characterized in that A) the acoustic oscillation (V 1 ) is transmitted to the sensor element (2) by the transmitter-receiver unit (3) at the first end (6) of the sensor element (2), wherein B) the first response (VV 1 ) of the acoustic oscillation (V 1 ) transmitted from the first end (6) and possibly reflected back from the measuring range of the sensor element (2) is received by the transmitter-receiver unit (3) at the first end (6) of said sensor element (2), the first response indicating a change in the state of water, wherein C) the second response (VV 2 ) of the acoustic oscillation (V) 1 transmitted from the first end is received at the second end (7) of the sensor element (2) of the transmitter-receiver unit (3), wherein D) the steps A to C are carried out so that acoustic oscillation (V 2 ) is transmitted from the second end (7) of the sensor element (2), whereby the responses (VV 3 , VV 4 ) of the acoustic oscillation (V 2 ) transmitted to the sensor element (2) are received according to steps B and C, wherein E) the steps A to C are repeated at certain intervals by alternating the transmitting end (6, 7) of the acoustic oscillation (V 1 , V 2 ), if necessary, and wherein F) the information from the transmitted oscillations (V 1 , V 2 ) and their responses (VV 1 , VV 2 ; VV 3 , VV 4 ) is used for calculating the state of water in the measuring range of the sensor element (2). Method according to any of claims 1 to 3, characterized in that particularly for the operations of the step (F) of claim 3, a central control unit (4) is arranged in connection with the transmitter-receiver unit (3), provided with a calculation programme for determining the information on the state of water, the calculation programme using groups of equations, at least one group of their variables consisting of said acoustic oscillations (V 1 , V 2 ) and their responses (VV 1 , VV 2 ; VV 3 , VV 4 ). Method according to any of claims 1 to 4, characterized in that the central control unit (4) is arranged to control operations on the structure (1), the sensor element (2) being in connection with the same, which are started on the basis of information on the state of water. Sensor arrangement for identification of different states of water on the surface of a structure (1), upon which at least a sensor element (2) of the sensor arrangement is placed, the sensor arrangement comprising: at least one longitudinal sensor element (2) made of a material conveying acoustic oscillation and a transmitter-receiver unit (3) coupled at the ends of the sensor element (2) for transmitting acoustic oscillation, preferably oscillation effective in the ultrasonic range, to the sensor element (2) and for receiving the response of the transmitted oscillation, characterized in that the transmitter-receiver unit (3) is arranged to transmit oscillation and to receive the corresponding response of the transmitted oscillation at both ends (6, 7) of the sensor element (2). Sensor arrangement according to claim 6, characterized in that the sensor element (2) is arranged to form a loop and that the transmitter-receiver unit (3) is a uniform unit. Sensor arrangement according to claim 6 or 7, characterized in that the loop-like sensor element (2) is placed on the first surface of the structure (1), that the transmitter-receiver unit (3) is placed on the side of the second surface of the structure (1), and that the sensor element (2) and the transmitter-receiver unit (3) are connected with each other by means of a lead-in arrangement (L 1 -L 4 ) penetrating the structure (1). Sensor arrangement according to any of claims 6 to 8, characterized in that the sensor element (2) is at least partly placed on a support (9), by means of which the sensor element (2) is at least partly fixed on the first surface of the structure (1). Sensor arrangement according to claim 9, characterized in that the support (9) is a longitudinal, flat form piece with means (9a) for fixing the sensor element (2) to the support. Sensor arrangement according to claim 9 or 10, characterized in that the bottom surface (10) of the longitudinal and flat form piece functioning as the support (9) is provided with said fixing and support means (9a) for fixing the sensor element (2), wherein the second bottom surface (11) is intended to be placed against the surface of the structure (1). Sensor arrangement according to claim 9 or 10, characterized in that in connection with or in the vicinity of at least one of the side edges of the longitudinal flat form piece functioning as the support (9), an arrangement of protruding parts (13) is provided, said fixing and support means (9a) for fixing the sensor element (2) being placed in connection with the same, wherein a space (13a, 13a') is left between the protruding parts (13), in which the sensor element (2) is exposed to fresh air. Sensor arrangement according to any of claims 10 to 12, characterized in that the fixing and support means (9a) and/or the positions of the lead-ins of the lead-in arrangement (L 1 -L 4 ) in the flat form piece functioning as the support (9) are so arranged that on at least part of the length of the sensor element (2), a parallel part (2a) is formed, in which the sections of the sensor element (2) are substantially aligned, at a distance from each other, said distance being defined by the fixing and support means (9a) of the support (9) and/or the lead-in arrangement (L 1 -L 4 ). Sensor arrangement according to any of claims 6 to 9, characterized in that the support, in which the sensor element (2) is placed, is formed by a substantially bar-like structure (15, 15a, 15b). Sensor arrangement according to claim 14, characterized in that the bar-like structure (15) comprises an inner opening (15c), wherein the first section (2') of the sensor element (2) is preferably wound around the bar-like structure (15) and the second section (2'') is led through the inner opening (12c) to the transmitter-receiver unit (3). Sensor arrangement according to claim 14, characterized in that the bar-like structure (15) is substantially U-formed, wherein the sensor element (2) is wound around the U-form to extend substantially on the whole length of the U-form. Sensor arrangement according to claim 8, 9 or 14, characterized in that the sensor element (2) is at least partly placed in connection with the structure (1), such as an aircraft wing, rotor or support structure (15), in a manner that it is in alignment with or overlapping the stagnation point of the structure (1) with a cross-sectional form of a wing profile. Sensor arrangement according to any of claims 14 to 17, characterized in that the support comprises further at least one plate (14, 14', 14'') or the like in connection with the bar-like structure (15; 15a, 15b), the sensor arrangement being arranged to be fixed to the structure (1) with fixing means in the plate (14, 14', 14''). Sensor arrangement according to claim 13, characterized in that the lead-in arrangement (L 1 -L 4 ) comprises a clamping device (KR) in connection with the hole (R) in the structure (1), its first element (TL) being fixed to the structure (1) and second element (LR) being fixed to the sensor element (2), wherein the first and second elements are, for clamping the sensor element (2), arranged to be movable in relation with each other and to be locked together with a locking device (L). Sensor arrangement according to any of claims 6 to 19, characterized in that in connection with the sensor arrangement, particularly the support (9, 15), means are arranged for changing and/or measuring physical conditions, such as heating and cooling units (16, 17) and/or at least one temperature measuring sensor (18).

Inventors: JOHANSSON REIJO, MAEKINEN JUHANI, WETZER PAUL, JOHANSSON, REIJO, MAEKINEN, JUHANI, WETZER, PAUL, Mäkinen, Juhani
Applicants: LABKO ICE DETECTION OY
Application year: 1994
Main classification: B64D15
IPC codes: G01N29, G01S5, G08B19, B64D15, G01V1, G01H17, G01H3